View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 31124U 26145.39097524 +.00000000 +00000-0 +87127-4 0 00000
2 31124 98.3479 119.8106 0046973 195.8246 164.1493 14.68126344 00
| Epoch (UTC): | 25 May 2026 09:23:00 |
| Eccentricity: | 0.0046973 |
| inclination: | 98.3479° |
| perigee height: | 634 km |
| apogee height: | 700 km |
| right ascension of ascending node: | 119.8106° |
| argument of perigee: | 195.8246° |
| revolutions per day: | 14.68126344 |
| mean anomaly at epoch: | 164.1493° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|